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学院简介：成果数量：8174

根据学校“强地、扬信、拓天”的发展战略，北京理工大学宇航学院于2008年12月30日正式组建。学院主要由具有悠久历史的航空宇航科学与技术和力学两个学科组成，航空宇航学科始建于 1957年，最初由火箭弹设计、推进剂及火工和制导专业组成。随后经过发展和调整，于1961年成立新的第一机械系，即飞行... [详细]

本院科研趋势：发文数量期刊收录

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[中文期刊] 带视场角限制的攻击时间控制制导律剑桥核源

作者：杨哲，林德福，王辉（北京理工大学宇航学院）

出处：系统工程与电子技术 2016 第38卷第9期 P2122-2128

关键词：多导弹；制导律；协同制导；攻击时间；视场角

摘要：为了实现多导弹协同攻击同一目标,根据弹目拦截几何关系,设计一种带有攻击时间控制及导引头视场限制的协同制导律。采用多项式函数推导含时间控制的导引指令,以附加反馈项的形式引入导引头视场角函数,实现对攻击时间及导引头视场角的同时约束。当已知导弹过载及导引头视场限制,导弹弹道轨迹可以由初始导弹参数确定,从而 ...

[中文会议论文] Autonomous Optical Navigation Approach Aided by Radio Beacon for Deep Space Spacecraft

作者： Jing Yan，Zhu Shengying，Wang Lina （School of Aerospace Engineering,Beijing Institute of Technology；Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration,Ministry of Industry and Information Technology；Key Laboratory of Dynamics and Control of Flight Vehicle Ministry of Education；National Key Laboratory of Science and Technology on Aerospace Intelligence Control）

出处：第28届中国控制与决策会议中国宁夏银川 2016

会议录：第28届中国控制与决策会议论文集（下）

摘要： According to task requests of deep space exploration approach phase such as autonomy,real-time and so on,we did a research into the problem of autonom ...

[中文期刊] 有多余坐标完整系统的自由运动^1）核源

作者：陈菊¹;吴惠彬²;梅凤翔¹; （¹北京理工大学宇航学院;²北京理工大学数学学院）

出处：力学学报 2016 第48卷第4期 P972-975

关键词：多余坐标；完整系统；约束力；自由运动

摘要：对于完整力学系统,若选取的参数不是完全独立的,则称为有多余坐标的完整系统.由于完整力学系统的第二类Lagrange方程中没有约束力,故为研究完整力学系统的约束力,需采用有多余坐标的带乘子的Lagrange方程或第一类Lagrange方程.一些动力学问题要求约束力不能为零,而另一些问题要求约束力很小. ...

[中文期刊] Optical flow based guidance system design for semi-strapdown image homing guided missiles 核源

作者： Huang Lan¹;Song Jianmei¹;Zhang Minqiang¹;Cai Gaohua²; （¹Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering,Beijing Institute of Technology;²Beijing Aerospace Automatic Control Institute）

出处：中国航空学报(英文版) 2016 第29卷第5期 P1345-1354

关键词： guidance；smoothed；missile；rotation；utilizing；coordinate；symmetric；translational；constraint；guided

摘要： This paper focuses mainly on semi-strapdown image homing guided(SSIHG) system design based on optical flow for a six-degree-of-freedom(6-DOF) axial-sy ...

[中文期刊] Space debris impact effects on Ultrasail dynamics CA 剑桥核

作者：李延艳¹;张景瑞¹;赵书阁²;杨科莹¹;关栋³;刘菲¹; （¹School of Aerospace Engineering,Beijing Institute of Technology;²The Second System Design Department of the Second Research Academy of China Aerospace Science and Industry Corporation;³School of Mechanical Engineering,Xi\'an Jiaotong University）

出处： Journal of Beijing Institute of Technology 2016 第A2期 P79-83

关键词： collision；analysis；Ultrasail；space；debris；LS-DYNA

摘要： The Ultrasail,a novel solar sail design development at the University of Illinois at UrbanaChampaign,relies in small-tip satellites to provide tension ...

[中文期刊] Experimental Investigation on Electromagnetic Attenuation by Low Pressure Radio-Frequency Plasma for Cavity Structure^∗ 核

作者：何湘¹;张亚春²;陈建平³;陈玉东³;曾小军³;姚洪^4,5;唐春梅¹; （¹School of Science, Hohai University;²School of Science, Nanjing University of Science & Technology;³Beijing Aeronautical Technology Research Center;⁴School of Aerospace Engineering, Beijing Institute of Technology;⁵Navy Logistics Department of PLA）

出处：等离子体科学和技术(英文版) 2016 第18卷第1期 P62-66

关键词： collision；transmitting；hollow；return；attenuation；cylinder；argon；inlet；filled；challenging

摘要： This paper reports on an experiment designed to test electromagnetic（EM）attenuation by radio-frequency（RF）plasma for cavity structures.A plasma reacto ...

[中文期刊] Stability analysis of a simple rheonomic nonholonomic constrained system 核源

作者：刘畅^1,2;刘世兴¹;梅凤翔³; （¹College of Physics,Liaoning University;²State Key Laboratory of Structural Analysis for Industrial Equipment,Department of Engineering Mechanics,Dalian University of Technology;³School of Aerospace Engineering,Beijing Institute of Technology）

出处： Chinese Physics B 2016 第25卷第12期 P318-321

关键词：非完整约束系统；稳定性分析；Lyapunov函数；运动微分方程；非完整力学系统；梯度系统；稳定性问题；非完整系统

摘要： It is a difficult problem to study the stability of the rheonomic and nonholonomic mechanical systems. Especially it is difficult to construct the Lya ...

[中文期刊] Surface Charging Controlling of the Chinese Space Station with Hollow Cathode Plasma Contactor 核

作者：蒋锴¹;王先荣¹;秦晓刚¹;杨生胜¹;杨威¹;赵呈选¹;陈益峰¹;史亮¹;汤道坦¹;谢侃²; （¹Science and Technology on Vacuum Technology and Physics Laboratory,Lanzhou Institute of Physics;²School of Aerospace Engineering, Beijing Institute of Technology）

出处：等离子体科学与技术(英文版) 2016 第18卷第7期 P727-731

关键词：充电控制；空心阴极；表面充电；等离子体；空间站；中国；接触器；太阳能电池阵列

摘要： A highly charged manned spacecraft threatens the life of an astronaut and extravehicular activity, which can be effectively reduced by controlling the ...

[外文期刊] Modal analysis and active vibration control of a cable-net reflector

作者： Wu Yongsheng¹;( winforever.wu@gmail.com);Zhang Weizhong¹;( hellowezwz@bit.edu.cn);Meng Xiuyun¹;( mengxy@bit.edu.cn) （¹Key Laboratory of Dynamics and Control of Flight Vehicles, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China）

出处： Applied Mechanics and Materials 2016 Vol.829 P137-143

关键词： Active vibration control;Cable-net reflector;LQR;Modal analysis

摘要： A cable-net reflector is first introduced and then the state space representation is derived based on the finite element model. Modal analysis is carr ...

[中文会议论文] Numerical Predictive Entry Guidance for Mars Low-Lifting Vehicles

作者： Rui Teng，Dong Qiao，Hongwei Han （School of Aerospace Engineering,Beijing Institute of Technology）

出处： 2016 IEEE Chinese Guidance, Navigation and Control Conference (IEEE CGNCC2016) 中国江苏南京 2016

会议录： Proceedings of 2016 IEEE Chinese Guidance, Navigation and Control Conference (IEEE CGNCC2016)

摘要： The Mars entry phase is very challenging during Mars landing process,and it is of great importance for Mars landing exploration mission.This paper con ...

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